Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rc08n1-il-200000-n5 Airfoil,rc08n1-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,56.7296 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-rc08n1-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.5881,0.09854,0.09536,0.0175,1.0000,0.0139 -8.250,-0.5862,0.09421,0.09106,0.0144,1.0000,0.0142 -8.000,-0.5847,0.08967,0.08656,0.0105,1.0000,0.0145 -7.500,-0.5772,0.07930,0.07617,-0.0015,1.0000,0.0154 -7.000,-0.4943,0.05791,0.05476,-0.0147,1.0000,0.0161 -6.750,-0.4971,0.05112,0.04792,-0.0155,1.0000,0.0166 -6.500,-0.4911,0.04618,0.04292,-0.0162,0.9874,0.0169 -6.250,-0.4770,0.04104,0.03763,-0.0177,0.9299,0.0174 -6.000,-0.4659,0.03688,0.03327,-0.0177,0.9051,0.0178 -5.750,-0.4542,0.03300,0.02918,-0.0172,0.8885,0.0184 -5.250,-0.4249,0.02570,0.02135,-0.0158,0.8646,0.0199 -5.000,-0.4077,0.02235,0.01768,-0.0148,0.8553,0.0204 -4.500,-0.3712,0.01671,0.01137,-0.0129,0.8390,0.0266 -4.000,-0.3434,0.02818,0.02174,-0.0093,0.8410,0.0311 -3.750,-0.3178,0.02439,0.01745,-0.0075,0.8341,0.0212 -3.500,-0.2921,0.02208,0.01477,-0.0065,0.8268,0.0201 -3.250,-0.2660,0.02020,0.01253,-0.0055,0.8205,0.0198 -3.000,-0.2390,0.01875,0.01082,-0.0049,0.8136,0.0205 -2.750,-0.2124,0.01791,0.00973,-0.0043,0.8074,0.0227 -2.500,-0.1855,0.01666,0.00828,-0.0038,0.8011,0.0224 -2.250,-0.1593,0.01562,0.00713,-0.0032,0.7950,0.0222 -2.000,-0.1334,0.01475,0.00618,-0.0027,0.7892,0.0222 -1.750,-0.1077,0.01402,0.00539,-0.0021,0.7829,0.0224 -1.500,-0.0824,0.01343,0.00472,-0.0016,0.7775,0.0227 -1.250,-0.0563,0.01294,0.00414,-0.0012,0.7709,0.0232 -1.000,-0.0306,0.01250,0.00359,-0.0007,0.7654,0.0250 -0.750,-0.0037,0.01221,0.00325,-0.0006,0.7588,0.0282 -0.500,0.0232,0.01203,0.00298,-0.0003,0.7529,0.0292 -0.250,0.0505,0.01190,0.00278,-0.0001,0.7466,0.0307 0.250,0.1046,0.01161,0.00251,0.0002,0.7333,0.0705 0.500,0.1189,0.00958,0.00238,0.0022,0.7264,0.6512 1.000,0.2351,0.00901,0.00262,-0.0096,0.7110,1.0000 1.250,0.2615,0.00903,0.00260,-0.0093,0.7021,1.0000 1.500,0.2876,0.00906,0.00256,-0.0090,0.6939,1.0000 1.750,0.3139,0.00909,0.00257,-0.0087,0.6846,1.0000 2.000,0.3402,0.00913,0.00260,-0.0085,0.6754,1.0000 2.250,0.3663,0.00917,0.00262,-0.0081,0.6664,1.0000 2.500,0.3924,0.00921,0.00265,-0.0078,0.6551,1.0000 2.750,0.4182,0.00924,0.00266,-0.0074,0.6385,1.0000 3.000,0.4438,0.00928,0.00269,-0.0068,0.6164,1.0000 3.250,0.4694,0.00935,0.00272,-0.0064,0.5944,1.0000 3.500,0.4950,0.00946,0.00278,-0.0059,0.5713,1.0000 3.750,0.5206,0.00959,0.00287,-0.0055,0.5430,1.0000 4.000,0.5458,0.00978,0.00301,-0.0050,0.5061,1.0000 4.250,0.5707,0.01006,0.00316,-0.0045,0.4594,1.0000 4.500,0.5947,0.01051,0.00337,-0.0040,0.3960,1.0000 4.750,0.6179,0.01117,0.00371,-0.0036,0.3196,1.0000 5.000,0.6406,0.01195,0.00416,-0.0033,0.2421,1.0000 5.250,0.6634,0.01271,0.00469,-0.0030,0.1784,1.0000 5.500,0.6862,0.01344,0.00523,-0.0026,0.1339,1.0000 5.750,0.7093,0.01411,0.00578,-0.0022,0.1040,1.0000 6.000,0.7327,0.01469,0.00633,-0.0017,0.0825,1.0000 6.250,0.7555,0.01536,0.00693,-0.0013,0.0640,1.0000 6.500,0.7784,0.01603,0.00765,-0.0007,0.0516,1.0000 6.750,0.8010,0.01673,0.00841,-0.0002,0.0421,1.0000 7.000,0.8234,0.01745,0.00921,0.0004,0.0343,1.0000 7.250,0.8439,0.01850,0.01029,0.0012,0.0287,1.0000 7.500,0.8654,0.01938,0.01134,0.0020,0.0256,1.0000 7.750,0.8869,0.02021,0.01226,0.0026,0.0217,1.0000 8.000,0.9045,0.02172,0.01389,0.0037,0.0186,1.0000 8.250,0.9244,0.02295,0.01532,0.0046,0.0170,1.0000 8.500,0.9437,0.02431,0.01687,0.0056,0.0151,1.0000 8.750,0.9640,0.02516,0.01784,0.0062,0.0128,1.0000 9.000,0.9779,0.02744,0.02030,0.0074,0.0111,1.0000 9.250,0.9935,0.02960,0.02275,0.0086,0.0104,1.0000 9.500,1.0079,0.03194,0.02543,0.0099,0.0097,1.0000 9.750,1.0193,0.03460,0.02850,0.0112,0.0091,1.0000 10.000,1.0294,0.03689,0.03111,0.0124,0.0082,1.0000 10.250,1.0399,0.03847,0.03290,0.0133,0.0074,1.0000 10.500,1.0494,0.03971,0.03425,0.0140,0.0068,1.0000 10.750,1.0491,0.04199,0.03671,0.0154,0.0064,1.0000 11.000,1.0380,0.04555,0.04055,0.0166,0.0062,1.0000 11.500,1.0097,0.05447,0.05000,0.0155,0.0060,1.0000 11.750,0.9951,0.05961,0.05537,0.0134,0.0060,1.0000 12.000,0.9788,0.06555,0.06153,0.0102,0.0060,1.0000 12.500,0.7834,0.08067,0.07728,0.0091,0.0090,1.0000 12.750,0.7553,0.09093,0.08762,0.0042,0.0095,1.0000